BG100519A - Propeller antivortical system - Google Patents
Propeller antivortical systemInfo
- Publication number
- BG100519A BG100519A BG100519A BG10051996A BG100519A BG 100519 A BG100519 A BG 100519A BG 100519 A BG100519 A BG 100519A BG 10051996 A BG10051996 A BG 10051996A BG 100519 A BG100519 A BG 100519A
- Authority
- BG
- Bulgaria
- Prior art keywords
- blade
- propeller
- tube
- nozzle
- formation
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/16—Drive of rotors by means, e.g. propellers, mounted on rotor blades
- B64C27/18—Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The system is used in aircraft engineering, in particular in helicopter making. It builds a reliable barrier against the formation of a "vortex ring" and has anti-icing effect. It consists of propeller blades (10) suspended on a propeller shaft (1). A tube (12) for gases under pressure fed by compressor (7) is passed inside each blade (10). End (15) of tube (12) reaches the external end (16) of propeller blade (10) where at least one nozzle (17) is mounted and to outlet (27) of blade (10) where there is a nozzle (28) at the end of each tube (16). Gas-fluid barriers (25 & 29) are formed by the flowing out of gases under pressure which do not allow the formation of a lateral turbulence and "vortical ring" above blade (10).
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BG100519A BG100519A (en) | 1996-04-19 | 1996-04-19 | Propeller antivortical system |
AU64103/96A AU6410396A (en) | 1996-04-19 | 1996-07-19 | An airscrew anti-eddy system |
PCT/BG1996/000009 WO1997039945A1 (en) | 1996-04-19 | 1996-07-19 | An airscrew anti-eddy system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BG100519A BG100519A (en) | 1996-04-19 | 1996-04-19 | Propeller antivortical system |
Publications (1)
Publication Number | Publication Date |
---|---|
BG100519A true BG100519A (en) | 1997-11-28 |
Family
ID=3926552
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BG100519A BG100519A (en) | 1996-04-19 | 1996-04-19 | Propeller antivortical system |
Country Status (3)
Country | Link |
---|---|
AU (1) | AU6410396A (en) |
BG (1) | BG100519A (en) |
WO (1) | WO1997039945A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103590920A (en) * | 2012-10-23 | 2014-02-19 | 摩尔动力(北京)技术股份有限公司 | Propeller |
CN103723274A (en) * | 2013-12-20 | 2014-04-16 | 华南农业大学 | Spraying device for rotorcraft and application thereof |
CN104149969B (en) * | 2014-08-26 | 2015-06-10 | 西北工业大学 | Propeller arrangement structure capable of achieving internally cooperative jet flow |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1001348A (en) * | 1946-04-20 | 1952-02-22 | Gen Mecanique Appliquee Soc In | Improvements to the means of driving, by reaction, of rotary openings propellers, in particular for helicopters |
US4655685A (en) * | 1985-12-16 | 1987-04-07 | United Technologies Corporation | Helicopter main rotor blade having a short span slot near the tip end |
-
1996
- 1996-04-19 BG BG100519A patent/BG100519A/en unknown
- 1996-07-19 AU AU64103/96A patent/AU6410396A/en not_active Abandoned
- 1996-07-19 WO PCT/BG1996/000009 patent/WO1997039945A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
AU6410396A (en) | 1997-11-12 |
WO1997039945A1 (en) | 1997-10-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA2038815A1 (en) | Device for separation of air from flotation slush | |
MY119874A (en) | Cyclonic separating apparatus | |
EP0258066A3 (en) | Method and apparatus of high speed machining | |
IE40105L (en) | Controlling the flow of pressurised fluid | |
EP0940338B1 (en) | Gearbox breather outlet | |
EP0935068A3 (en) | Device to funnel fluid flow into a turbine | |
SE430307B (en) | DEVICE FOR INJECTION OF GAS AND USE OF LIQUIDS | |
BG100519A (en) | Propeller antivortical system | |
CA2336765A1 (en) | Air-pressure head | |
BR9705181A (en) | Water jet system | |
US4111671A (en) | Method and apparatus for carbon dioxide snow separation | |
SE452413B (en) | MEDIUM MIXING NOZE, INTENDED TO BE USED IN A CONTACT REACTOR | |
AU9267598A (en) | Propulsion system and method | |
JPH0423039B2 (en) | ||
EP0930432A3 (en) | Rotor blade form for Francis water turbine | |
WO2000061918A3 (en) | Airfoil leading edge vortex elimination device | |
ATE120388T1 (en) | WIND SIFTER. | |
NL7705793A (en) | Wind energy recovery unit - comprises open ducts with hexagonal ends and round throats, accommodating propellers | |
US4655090A (en) | Turbine flowmeter for fluids | |
RU95106564A (en) | Lifting surface | |
NO895192D0 (en) | INSTALLATIONS FOR AA REDUCE THE TENDENCE OF KAVITION EROSION PROPELLER. | |
JPS57370A (en) | Conical streamer | |
DE3760395D1 (en) | Double tangential nozzle | |
JPS5447916A (en) | Variable capacity nozzleless turbine | |
GB1509149A (en) | Device for preparing fibre-filled polymeric compositions |